page_title: Wibault 170 Tornade
section_title: Specifications (Wib 170 Tornade)
hierarchical_section_title: Wibault 170 Tornade / Specifications (Wib 170 Tornade)
caption_attribution_description: English: Wibault 13 C.1 3-view drawing from L'Air April 15,1928
context_page_description: The Wibault 13C.1 Trombe, later known as the Wib 130C.1 Trombe was a single seat, parasol wing lightweight fighter aircraft designed and built in France in the 1920s. It was developed into the more powerful Wib 170C.1 Tornade but government interest in lightweight fighters soon waned.
context_section_description: Data from Green & Swanborough p.597
  General characteristics
  Crew: One
  Length: 7.15 m (23 ft 5 in)
  Wingspan: 9.07 m (29 ft 9 in)
  Height: 2.77 m (9 ft 1 in)
  Wing area: 17.00 m² (183.0 sq ft)
  Empty weight: 965 kg (2,127 lb)
  Gross weight: 1,350 kg (2,976 lb)
  Fuel capacity: 300 L (66 UKgal, 79 USgal)
  Powerplant: 1 × Hispano-Suiza 12Hb water-cooled upright V-12, 370 kW (500 hp)
  Propellers: 2-bladed
  Performance
  Maximum speed: 279 km/h (173 mph, 151 kn) at sea level
  Service ceiling: 9,600 m (31,500 ft)
  Time to altitude: 9.15 min to 5,000 m (16,405 ft)
  Armament
  Fuselage guns 2×7.7 mm (0.303 in) synchronised Vickers machine guns firing through the propeller arc.
caption: Wibault 13 C.1 3-view drawing from L'Air April 15,1928
exif: {}